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 63207U 26087.54376713 +.00000000 +00000-0 +45100-3 0 00003
2 63207 42.0173 185.5546 0005057 289.9962 70.0320 15.02732654 00
| Epoch (UTC): | 28 March 2026 13:03:01 |
| Eccentricity: | 0.0005057 |
| inclination: | 42.0173° |
| perigee height: | 555 km |
| apogee height: | 562 km |
| right ascension of ascending node: | 185.5546° |
| argument of perigee: | 289.9962° |
| revolutions per day: | 15.02732654 |
| mean anomaly at epoch: | 70.0320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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