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 50501U 26145.48858633 +.00000000 +00000-0 -26752-2 0 00002
2 50501 87.9162 339.9754 0001607 91.4672 268.6644 13.18691119 05
| Epoch (UTC): | 25 May 2026 11:43:33 |
| Eccentricity: | 0.0001607 |
| inclination: | 87.9162° |
| perigee height: | 1189 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9754° |
| argument of perigee: | 91.4672° |
| revolutions per day: | 13.18691119 |
| mean anomaly at epoch: | 268.6644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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