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 66286U 26145.43224053 +.00000000 +00000-0 +14029-3 0 00001
2 66286 53.1575 194.9536 0001236 100.3000 259.8140 15.30209222 04
| Epoch (UTC): | 25 May 2026 10:22:25 |
| Eccentricity: | 0.0001236 |
| inclination: | 53.1575° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 194.9536° |
| argument of perigee: | 100.3000° |
| revolutions per day: | 15.30209222 |
| mean anomaly at epoch: | 259.8140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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