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 51636U 26145.57563486 +.00000000 +00000-0 -60045-3 0 00005
2 51636 87.9155 10.3750 0002305 93.4938 266.6457 13.17648516 08
| Epoch (UTC): | 25 May 2026 13:48:54 |
| Eccentricity: | 0.0002305 |
| inclination: | 87.9155° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3750° |
| argument of perigee: | 93.4938° |
| revolutions per day: | 13.17648516 |
| mean anomaly at epoch: | 266.6457° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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