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 53900U 26145.55450847 +.00000000 +00000-0 -15445-4 0 00000
2 53900 53.2154 338.6999 0001424 89.3229 270.7926 15.08832543 02
| Epoch (UTC): | 25 May 2026 13:18:29 |
| Eccentricity: | 0.0001424 |
| inclination: | 53.2154° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 338.6999° |
| argument of perigee: | 89.3229° |
| revolutions per day: | 15.08832543 |
| mean anomaly at epoch: | 270.7926° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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