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 26044.42328659 +.00000000 +00000-0 +11953-3 0 00002
2 02802 74.0106 33.4050 0063256 45.7042 314.9279 14.45597570 03
| Epoch (UTC): | 13 February 2026 10:09:31 |
| Eccentricity: | 0.0063256 |
| inclination: | 74.0106° |
| perigee height: | 695 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 33.4050° |
| argument of perigee: | 45.7042° |
| revolutions per day: | 14.45597570 |
| mean anomaly at epoch: | 314.9279° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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