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 48951U 26145.26116955 +.00000000 +00000-0 +31790-3 0 00006
2 48951 97.7041 336.9513 0008129 75.0657 285.1496 15.54012480 02
| Epoch (UTC): | 25 May 2026 06:16:05 |
| Eccentricity: | 0.0008129 |
| inclination: | 97.7041° |
| perigee height: | 400 km |
| apogee height: | 411 km |
| right ascension of ascending node: | 336.9513° |
| argument of perigee: | 75.0657° |
| revolutions per day: | 15.54012480 |
| mean anomaly at epoch: | 285.1496° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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