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 52648U 26145.35996613 +.00000000 +00000-0 -22743-3 0 00000
2 52648 53.2137 274.9334 0001530 84.4061 275.7106 15.08853235 00
| Epoch (UTC): | 25 May 2026 08:38:21 |
| Eccentricity: | 0.0001530 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 274.9334° |
| argument of perigee: | 84.4061° |
| revolutions per day: | 15.08853235 |
| mean anomaly at epoch: | 275.7106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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