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 49292U 26145.37218578 +.00000000 +00000-0 -23750-3 0 00009
2 49292 87.8938 294.2570 0001860 98.9117 261.2223 13.14501613 03
| Epoch (UTC): | 25 May 2026 08:55:56 |
| Eccentricity: | 0.0001860 |
| inclination: | 87.8938° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2570° |
| argument of perigee: | 98.9117° |
| revolutions per day: | 13.14501613 |
| mean anomaly at epoch: | 261.2223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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