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 59877U 26145.41726903 +.00000000 +00000-0 +69400-5 0 00003
2 59877 43.0003 200.9620 0001392 259.4172 100.6522 15.27574205 06
| Epoch (UTC): | 25 May 2026 10:00:52 |
| Eccentricity: | 0.0001392 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.9620° |
| argument of perigee: | 259.4172° |
| revolutions per day: | 15.27574205 |
| mean anomaly at epoch: | 100.6522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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