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 66667U 26145.17632035 +.00000000 +00000-0 +16090-3 0 00008
2 66667 97.4124 220.2285 0004603 70.8355 289.3382 15.28858512 02
| Epoch (UTC): | 25 May 2026 04:13:54 |
| Eccentricity: | 0.0004603 |
| inclination: | 97.4124° |
| perigee height: | 476 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 220.2285° |
| argument of perigee: | 70.8355° |
| revolutions per day: | 15.28858512 |
| mean anomaly at epoch: | 289.3382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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