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 66243U 26145.38932056 +.00000000 +00000-0 +75580-3 0 00006
2 66243 53.1594 287.3453 0001788 75.5805 284.5394 15.30212684 03
| Epoch (UTC): | 25 May 2026 09:20:37 |
| Eccentricity: | 0.0001788 |
| inclination: | 53.1594° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 287.3453° |
| argument of perigee: | 75.5805° |
| revolutions per day: | 15.30212684 |
| mean anomaly at epoch: | 284.5394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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