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 54861U 26145.12215084 +.00000000 +00000-0 +32087-4 0 00002
2 54861 43.0055 49.6212 0001184 266.3114 93.7602 15.27575631 03
| Epoch (UTC): | 25 May 2026 02:55:53 |
| Eccentricity: | 0.0001184 |
| inclination: | 43.0055° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 49.6212° |
| argument of perigee: | 266.3114° |
| revolutions per day: | 15.27575631 |
| mean anomaly at epoch: | 93.7602° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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