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 54823U 26145.18060889 +.00000000 +00000-0 +29099-4 0 00006
2 54823 43.0050 63.9122 0001154 259.1793 100.8929 15.27578232 07
| Epoch (UTC): | 25 May 2026 04:20:04 |
| Eccentricity: | 0.0001154 |
| inclination: | 43.0050° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 63.9122° |
| argument of perigee: | 259.1793° |
| revolutions per day: | 15.27578232 |
| mean anomaly at epoch: | 100.8929° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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