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 53052U 26145.38459235 +.00000000 +00000-0 +15800-2 0 00001
2 53052 97.4474 325.2870 0001879 189.0354 171.0840 15.05545060 06
| Epoch (UTC): | 25 May 2026 09:13:48 |
| Eccentricity: | 0.0001879 |
| inclination: | 97.4474° |
| perigee height: | 549 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 325.2870° |
| argument of perigee: | 189.0354° |
| revolutions per day: | 15.05545060 |
| mean anomaly at epoch: | 171.0840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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