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 52111U 26145.25508735 +.00000000 +00000-0 +14711-4 0 00004
2 52111 53.2151 95.4038 0001502 99.7826 260.3335 15.08840590 09
| Epoch (UTC): | 25 May 2026 06:07:19 |
| Eccentricity: | 0.0001502 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 95.4038° |
| argument of perigee: | 99.7826° |
| revolutions per day: | 15.08840590 |
| mean anomaly at epoch: | 260.3335° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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