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 26076.26538789 +.00000000 +00000-0 +81820-4 0 00002
2 02825 69.9701 270.8873 0009643 285.0872 74.9167 13.97710906 07
| Epoch (UTC): | 17 March 2026 06:22:09 |
| Eccentricity: | 0.0009643 |
| inclination: | 69.9701° |
| perigee height: | 895 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 270.8873° |
| argument of perigee: | 285.0872° |
| revolutions per day: | 13.97710906 |
| mean anomaly at epoch: | 74.9167° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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