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 52995U 26145.20035580 +.00000000 +00000-0 +72729-5 0 00006
2 52995 53.2138 110.6476 0001801 63.0487 297.0689 15.08839805 05
| Epoch (UTC): | 25 May 2026 04:48:30 |
| Eccentricity: | 0.0001801 |
| inclination: | 53.2138° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 110.6476° |
| argument of perigee: | 63.0487° |
| revolutions per day: | 15.08839805 |
| mean anomaly at epoch: | 297.0689° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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