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 54690U 26145.62750617 +.00000000 +00000-0 +31087-3 0 00001
2 54690 97.6815 312.5615 0005766 173.4520 186.6798 15.33960282 05
| Epoch (UTC): | 25 May 2026 15:03:36 |
| Eccentricity: | 0.0005766 |
| inclination: | 97.6815° |
| perigee height: | 460 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 312.5615° |
| argument of perigee: | 173.4520° |
| revolutions per day: | 15.33960282 |
| mean anomaly at epoch: | 186.6798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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