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 53254U 26145.41290495 +.00000000 +00000-0 -56837-4 0 00008
2 53254 53.2110 209.7060 0001307 91.8252 268.2889 15.08843262 07
| Epoch (UTC): | 25 May 2026 09:54:34 |
| Eccentricity: | 0.0001307 |
| inclination: | 53.2110° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 209.7060° |
| argument of perigee: | 91.8252° |
| revolutions per day: | 15.08843262 |
| mean anomaly at epoch: | 268.2889° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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