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 02873U 26087.78329757 +.00000000 +00000-0 +88261-4 0 00003
2 02873 69.9739 222.8529 0010479 260.7120 207.8606 13.98508826 03
| Epoch (UTC): | 28 March 2026 18:47:56 |
| Eccentricity: | 0.0010479 |
| inclination: | 69.9739° |
| perigee height: | 891 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 222.8529° |
| argument of perigee: | 260.7120° |
| revolutions per day: | 13.98508826 |
| mean anomaly at epoch: | 207.8606° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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