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 55046U 26145.61180728 +.00000000 +00000-0 +30887-3 0 00003
2 55046 97.3216 205.9798 0007876 186.6574 173.4567 15.35747710 08
| Epoch (UTC): | 25 May 2026 14:41:00 |
| Eccentricity: | 0.0007876 |
| inclination: | 97.3216° |
| perigee height: | 453 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 205.9798° |
| argument of perigee: | 186.6574° |
| revolutions per day: | 15.35747710 |
| mean anomaly at epoch: | 173.4567° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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