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 54082U 26145.60885103 +.00000000 +00000-0 +48333-4 0 00006
2 54082 53.2118 349.0022 0001306 97.2638 262.8502 15.08839348 00
| Epoch (UTC): | 25 May 2026 14:36:44 |
| Eccentricity: | 0.0001306 |
| inclination: | 53.2118° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 349.0022° |
| argument of perigee: | 97.2638° |
| revolutions per day: | 15.08839348 |
| mean anomaly at epoch: | 262.8502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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