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 55800U 26145.64236152 +.00000000 +00000-0 +24881-3 0 00004
2 55800 87.9165 278.9776 0001711 93.6675 266.4654 13.20770971 08
| Epoch (UTC): | 25 May 2026 15:25:00 |
| Eccentricity: | 0.0001711 |
| inclination: | 87.9165° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9776° |
| argument of perigee: | 93.6675° |
| revolutions per day: | 13.20770971 |
| mean anomaly at epoch: | 266.4654° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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