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 52633U 26145.40320707 +.00000000 +00000-0 +53050-5 0 00001
2 52633 53.2139 284.7405 0001239 81.2910 278.8223 15.08837928 03
| Epoch (UTC): | 25 May 2026 09:40:37 |
| Eccentricity: | 0.0001239 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 284.7405° |
| argument of perigee: | 81.2910° |
| revolutions per day: | 15.08837928 |
| mean anomaly at epoch: | 278.8223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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