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 02825U 26076.05069580 +.00000000 +00000-0 +85136-4 0 00001
2 02825 69.9701 271.3484 0009632 285.1847 74.8194 13.97710882 04
| Epoch (UTC): | 17 March 2026 01:13:00 |
| Eccentricity: | 0.0009632 |
| inclination: | 69.9701° |
| perigee height: | 895 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 271.3484° |
| argument of perigee: | 285.1847° |
| revolutions per day: | 13.97710882 |
| mean anomaly at epoch: | 74.8194° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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