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 52875U 26145.39171176 +.00000000 +00000-0 +92387-4 0 00006
2 52875 53.2124 29.7898 0001556 88.9667 271.1503 15.08832599 09
| Epoch (UTC): | 25 May 2026 09:24:03 |
| Eccentricity: | 0.0001556 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 29.7898° |
| argument of perigee: | 88.9667° |
| revolutions per day: | 15.08832599 |
| mean anomaly at epoch: | 271.1503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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