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 66129U 26145.13952905 +.00000000 +00000-0 +11584-2 0 00000
2 66129 53.1589 44.6427 0000846 80.7475 279.3621 15.30209115 00
| Epoch (UTC): | 25 May 2026 03:20:55 |
| Eccentricity: | 0.0000846 |
| inclination: | 53.1589° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 44.6427° |
| argument of perigee: | 80.7475° |
| revolutions per day: | 15.30209115 |
| mean anomaly at epoch: | 279.3621° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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