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 50480U 26145.47341015 +.00000000 +00000-0 +20403-4 0 00006
2 50480 87.9169 339.9644 0001712 93.1803 266.9525 13.18688262 02
| Epoch (UTC): | 25 May 2026 11:21:42 |
| Eccentricity: | 0.0001712 |
| inclination: | 87.9169° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9644° |
| argument of perigee: | 93.1803° |
| revolutions per day: | 13.18688262 |
| mean anomaly at epoch: | 266.9525° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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