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 66397U 26145.60396378 +.00000000 +00000-0 +42297-3 0 00001
2 66397 53.1584 219.4621 0001212 72.5559 287.5574 15.30202536 08
| Epoch (UTC): | 25 May 2026 14:29:42 |
| Eccentricity: | 0.0001212 |
| inclination: | 53.1584° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 219.4621° |
| argument of perigee: | 72.5559° |
| revolutions per day: | 15.30202536 |
| mean anomaly at epoch: | 287.5574° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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