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 20253U 26145.46600691 +.00000000 +00000-0 +00000-0 0 00005
2 20253 12.4280 351.3022 0005977 30.2313 154.8795 1.00265798 04
| Epoch (UTC): | 25 May 2026 11:11:02 |
| Eccentricity: | 0.0005977 |
| inclination: | 12.4280° |
| perigee height: | 35763 km |
| apogee height: | 35813 km |
| right ascension of ascending node: | 351.3022° |
| argument of perigee: | 30.2313° |
| revolutions per day: | 1.00265798 |
| mean anomaly at epoch: | 154.8795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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