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 53807U 26130.49007553 +.00000000 +00000-0 +11053-3 0 00004
2 53807 53.2285 210.8807 0007320 64.2299 295.9461 15.37820008 00
| Epoch (UTC): | 10 May 2026 11:45:42 |
| Eccentricity: | 0.0007320 |
| inclination: | 53.2285° |
| perigee height: | 448 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 210.8807° |
| argument of perigee: | 64.2299° |
| revolutions per day: | 15.37820008 |
| mean anomaly at epoch: | 295.9461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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