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 50001U 26145.25595236 +.00000000 +00000-0 +00000-0 0 00004
2 50001 0.0199 295.4345 0000284 31.4571 153.1008 1.00271491 07
| Epoch (UTC): | 25 May 2026 06:08:34 |
| Eccentricity: | 0.0000284 |
| inclination: | 0.0199° |
| perigee height: | 35785 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 295.4345° |
| argument of perigee: | 31.4571° |
| revolutions per day: | 1.00271491 |
| mean anomaly at epoch: | 153.1008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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