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 25157U 26103.94292479 +.00000000 +00000-0 +41327-3 0 00001
2 25157 108.0123 356.8479 0039168 116.5317 243.9917 15.71413062 05
| Epoch (UTC): | 13 April 2026 22:37:48 |
| Eccentricity: | 0.0039168 |
| inclination: | 108.0123° |
| perigee height: | 328 km |
| apogee height: | 381 km |
| right ascension of ascending node: | 356.8479° |
| argument of perigee: | 116.5317° |
| revolutions per day: | 15.71413062 |
| mean anomaly at epoch: | 243.9917° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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