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 25477U 26088.08988882 +.00000000 +00000-0 +38874-3 0 00006
2 25477 45.0099 1.1954 0001764 246.0444 114.0220 14.38321883 07
| Epoch (UTC): | 29 March 2026 02:09:26 |
| Eccentricity: | 0.0001764 |
| inclination: | 45.0099° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 1.1954° |
| argument of perigee: | 246.0444° |
| revolutions per day: | 14.38321883 |
| mean anomaly at epoch: | 114.0220° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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