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 50477U 26145.49534469 +.00000000 +00000-0 +62946-4 0 00009
2 50477 87.9169 339.9702 0002050 85.1319 275.0047 13.18687706 04
| Epoch (UTC): | 25 May 2026 11:53:17 |
| Eccentricity: | 0.0002050 |
| inclination: | 87.9169° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9702° |
| argument of perigee: | 85.1319° |
| revolutions per day: | 13.18687706 |
| mean anomaly at epoch: | 275.0047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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