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 66076U 26145.00844884 +.00000000 +00000-0 +65979-3 0 00001
2 66076 53.1597 250.9608 0001158 84.1288 275.9845 15.30201496 04
| Epoch (UTC): | 25 May 2026 00:12:09 |
| Eccentricity: | 0.0001158 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 250.9608° |
| argument of perigee: | 84.1288° |
| revolutions per day: | 15.30201496 |
| mean anomaly at epoch: | 275.9845° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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