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 53109U 26145.46138204 +.00000000 +00000-0 +00000-0 0 00007
2 53109 70.1431 306.1510 0008884 295.0612 64.9126 6.42583293 05
| Epoch (UTC): | 25 May 2026 11:04:23 |
| Eccentricity: | 0.0008884 |
| inclination: | 70.1431° |
| perigee height: | 5832 km |
| apogee height: | 5854 km |
| right ascension of ascending node: | 306.1510° |
| argument of perigee: | 295.0612° |
| revolutions per day: | 6.42583293 |
| mean anomaly at epoch: | 64.9126° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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