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 48957U 26145.48540716 +.00000000 +00000-0 +36119-3 0 00002
2 48957 97.6753 342.9509 0005588 65.1084 295.0756 15.67501656 00
| Epoch (UTC): | 25 May 2026 11:38:59 |
| Eccentricity: | 0.0005588 |
| inclination: | 97.6753° |
| perigee height: | 362 km |
| apogee height: | 370 km |
| right ascension of ascending node: | 342.9509° |
| argument of perigee: | 65.1084° |
| revolutions per day: | 15.67501656 |
| mean anomaly at epoch: | 295.0756° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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