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 48931U 26145.48583860 +.00000000 +00000-0 +36030-3 0 00003
2 48931 97.6684 340.0813 0005264 63.9204 296.2597 15.67504363 07
| Epoch (UTC): | 25 May 2026 11:39:36 |
| Eccentricity: | 0.0005264 |
| inclination: | 97.6684° |
| perigee height: | 362 km |
| apogee height: | 370 km |
| right ascension of ascending node: | 340.0813° |
| argument of perigee: | 63.9204° |
| revolutions per day: | 15.67504363 |
| mean anomaly at epoch: | 296.2597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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