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 00604U 63024 A 94152.18073690 .02129576 +52585-4 +43933-3 06960
2 00604 058.1709 094.7046 0005086 284.1902 076.0350 16.30524975692579
| Epoch (UTC): | 01 June 1994 04:20:15 |
| Eccentricity: | 0.0005086 |
| inclination: | 58.1709° |
| perigee height: | 188 km |
| apogee height: | 194 km |
| right ascension of ascending node: | 94.7046° |
| argument of perigee: | 284.1902° |
| revolutions per day: | 16.30524975 |
| mean anomaly at epoch: | 76.0350° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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