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 53848U 26145.45055597 +.00000000 +00000-0 +44186-4 0 00006
2 53848 53.2118 309.2632 0001073 87.8253 272.2862 15.08837788 03
| Epoch (UTC): | 25 May 2026 10:48:48 |
| Eccentricity: | 0.0001073 |
| inclination: | 53.2118° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 309.2632° |
| argument of perigee: | 87.8253° |
| revolutions per day: | 15.08837788 |
| mean anomaly at epoch: | 272.2862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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