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 52490U 26145.46761919 +.00000000 +00000-0 +33289-4 0 00003
2 52490 53.2115 64.4497 0001214 93.2156 266.8975 15.08823694 06
| Epoch (UTC): | 25 May 2026 11:13:22 |
| Eccentricity: | 0.0001214 |
| inclination: | 53.2115° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 64.4497° |
| argument of perigee: | 93.2156° |
| revolutions per day: | 15.08823694 |
| mean anomaly at epoch: | 266.8975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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