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 50499U 26145.51388972 +.00000000 +00000-0 -11714-4 0 00000
2 50499 87.9170 339.9462 0002020 92.6490 267.4873 13.18686595 00
| Epoch (UTC): | 25 May 2026 12:20:00 |
| Eccentricity: | 0.0002020 |
| inclination: | 87.9170° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9462° |
| argument of perigee: | 92.6490° |
| revolutions per day: | 13.18686595 |
| mean anomaly at epoch: | 267.4873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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