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 66806U 26145.05137965 +.00000000 +00000-0 +69368-3 0 00008
2 66806 43.0052 43.4646 0001888 279.6808 80.3831 15.27586072 00
| Epoch (UTC): | 25 May 2026 01:13:59 |
| Eccentricity: | 0.0001888 |
| inclination: | 43.0052° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 43.4646° |
| argument of perigee: | 279.6808° |
| revolutions per day: | 15.27586072 |
| mean anomaly at epoch: | 80.3831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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