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 53003U 26145.63459689 +.00000000 +00000-0 +40379-3 0 00008
2 53003 53.2131 108.6986 0001254 91.9155 268.1981 15.08813686 09
| Epoch (UTC): | 25 May 2026 15:13:49 |
| Eccentricity: | 0.0001254 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 108.6986° |
| argument of perigee: | 91.9155° |
| revolutions per day: | 15.08813686 |
| mean anomaly at epoch: | 268.1981° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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