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 02802U 26041.44754027 +.00000000 +00000-0 +10794-3 0 00005
2 02802 74.0103 38.9626 0063136 52.0645 308.6195 14.45595013 03
| Epoch (UTC): | 10 February 2026 10:44:27 |
| Eccentricity: | 0.0063136 |
| inclination: | 74.0103° |
| perigee height: | 695 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 38.9626° |
| argument of perigee: | 52.0645° |
| revolutions per day: | 14.45595013 |
| mean anomaly at epoch: | 308.6195° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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