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 25117U 26100.18803772 +.00000000 +00000-0 +44194-3 0 00009
2 25117 45.0154 20.6609 0003064 306.1526 53.9042 14.47207181 04
| Epoch (UTC): | 10 April 2026 04:30:46 |
| Eccentricity: | 0.0003064 |
| inclination: | 45.0154° |
| perigee height: | 733 km |
| apogee height: | 737 km |
| right ascension of ascending node: | 20.6609° |
| argument of perigee: | 306.1526° |
| revolutions per day: | 14.47207181 |
| mean anomaly at epoch: | 53.9042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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