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 53894U 26145.66668980 +.00000000 +00000-0 +14019-2 0 00006
2 53894 53.2184 336.6531 0001117 91.9766 242.8107 15.28997111 07
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001117 |
| inclination: | 53.2184° |
| perigee height: | 478 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 336.6531° |
| argument of perigee: | 91.9766° |
| revolutions per day: | 15.28997111 |
| mean anomaly at epoch: | 242.8107° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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