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 55816U 26145.38964366 +.00000000 +00000-0 +47162-3 0 00004
2 55816 87.8938 294.2516 0002202 98.7985 261.3394 13.14502602 03
| Epoch (UTC): | 25 May 2026 09:21:05 |
| Eccentricity: | 0.0002202 |
| inclination: | 87.8938° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2516° |
| argument of perigee: | 98.7985° |
| revolutions per day: | 13.14502602 |
| mean anomaly at epoch: | 261.3394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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