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 53802U 26145.36501183 +.00000000 +00000-0 -50617-4 0 00000
2 53802 53.2146 279.7764 0000998 110.5419 249.5680 15.08830107 07
| Epoch (UTC): | 25 May 2026 08:45:37 |
| Eccentricity: | 0.0000998 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 279.7764° |
| argument of perigee: | 110.5419° |
| revolutions per day: | 15.08830107 |
| mean anomaly at epoch: | 249.5680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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