Spacecraft information: DODECAPOLE 2
| Launched | 12 August 1965 |
| Flight ended | – |
| Status | Unknown |
| Launch site | Air Force Western Test Range, California, USA |
| Owner | United States |
| NORAD ID | 1510 |
| COSPAR ID | 1965-065C |
| Observing |
Current orbital elements
| Inclination | 90.066° |
| Eccentricity | 0.00411 |
| RA ascending node | 1.681 hr |
| Argument perigee | 92.206° |
| Mean anomaly | 268.382° |
| Orbital period | 102.029 min |
| Epoch of osculation | 16 Jul 2026, 06:20 |
Derived Quantities
| Min Altitude | 832.2 km |
| Mean Altitude | 861.9 km |
| Peak Altitude | 891.6 km |
Launched alongside
THOR ABLESTAR DEB THOR ABLESTAR R/B THOR ABLESTAR DEB TEMPSAT 1 OPS 8464 NAVSPASUR ROD 1 CALSPHERE 4A THOR ABLESTAR DEB THOR ABLESTAR DEB PORCUPINE 2 OPS 8464 DEB TRANSIT 5B-7 DEB THOR ABLESTAR DEB THOR ABLESTAR DEB THOR ABLESTAR DEB THOR ABLESTAR DEB TRANSIT 5B-7 DEB DODECAPOLE 2 DEBOrbital History
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