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 26106.55280728 +.00000000 +00000-0 +40024-3 0 00008
2 25157 108.0117 3.4975 0038864 110.8004 249.7376 15.71688603 04
| Epoch (UTC): | 16 April 2026 13:16:02 |
| Eccentricity: | 0.0038864 |
| inclination: | 108.0117° |
| perigee height: | 328 km |
| apogee height: | 380 km |
| right ascension of ascending node: | 3.4975° |
| argument of perigee: | 110.8004° |
| revolutions per day: | 15.71688603 |
| mean anomaly at epoch: | 249.7376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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