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 53745U 26145.40920708 +.00000000 +00000-0 +31880-5 0 00000
2 53745 53.2150 279.8375 0001250 83.4659 276.6475 15.08834879 06
| Epoch (UTC): | 25 May 2026 09:49:15 |
| Eccentricity: | 0.0001250 |
| inclination: | 53.2150° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 279.8375° |
| argument of perigee: | 83.4659° |
| revolutions per day: | 15.08834879 |
| mean anomaly at epoch: | 276.6475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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