View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 04553U 70075 A 70274.48256745 .00177095 +00000-0 +00000-0 0 00076
2 04553 065.4336 142.3308 0081090 051.7015 309.1367 16.09111603001440
| Epoch (UTC): | 01 October 1970 11:34:53 |
| Eccentricity: | 0.0081090 |
| inclination: | 65.4336° |
| perigee height: | 195 km |
| apogee height: | 303 km |
| right ascension of ascending node: | 142.3308° |
| argument of perigee: | 51.7015° |
| revolutions per day: | 16.09111603 |
| mean anomaly at epoch: | 309.1367° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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