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 53981U 26145.57660314 +.00000000 +00000-0 +40226-4 0 00007
2 53981 53.2129 218.7375 0001238 96.7568 263.3565 15.08834973 06
| Epoch (UTC): | 25 May 2026 13:50:18 |
| Eccentricity: | 0.0001238 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 218.7375° |
| argument of perigee: | 96.7568° |
| revolutions per day: | 15.08834973 |
| mean anomaly at epoch: | 263.3565° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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