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 54834U 26145.48583602 +.00000000 +00000-0 +38832-4 0 00009
2 54834 43.0067 62.7536 0001517 266.9195 93.1483 15.27579239 05
| Epoch (UTC): | 25 May 2026 11:39:36 |
| Eccentricity: | 0.0001517 |
| inclination: | 43.0067° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 62.7536° |
| argument of perigee: | 266.9195° |
| revolutions per day: | 15.27579239 |
| mean anomaly at epoch: | 93.1483° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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