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 52635U 26145.38572794 +.00000000 +00000-0 -33990-4 0 00006
2 52635 53.2140 274.8156 0001307 96.8175 263.2966 15.08842571 03
| Epoch (UTC): | 25 May 2026 09:15:26 |
| Eccentricity: | 0.0001307 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 274.8156° |
| argument of perigee: | 96.8175° |
| revolutions per day: | 15.08842571 |
| mean anomaly at epoch: | 263.2966° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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