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 66542U 26145.55536612 +.00000000 +00000-0 +76202-3 0 00007
2 66542 43.0003 204.3103 0001409 305.3047 54.7673 15.27572856 04
| Epoch (UTC): | 25 May 2026 13:19:43 |
| Eccentricity: | 0.0001409 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.3103° |
| argument of perigee: | 305.3047° |
| revolutions per day: | 15.27572856 |
| mean anomaly at epoch: | 54.7673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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