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 25273U 26088.09972176 +.00000000 +00000-0 +12225-3 0 00002
2 25273 86.3999 25.7570 0002081 89.7228 270.4207 14.36139509 01
| Epoch (UTC): | 29 March 2026 02:23:35 |
| Eccentricity: | 0.0002081 |
| inclination: | 86.3999° |
| perigee height: | 770 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 25.7570° |
| argument of perigee: | 89.7228° |
| revolutions per day: | 14.36139509 |
| mean anomaly at epoch: | 270.4207° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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