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 41725U 26145.31864316 +.00000000 +00000-0 +00000-0 0 00002
2 41725 3.8075 43.2388 0006357 34.3757 21.4207 1.00270446 02
| Epoch (UTC): | 25 May 2026 07:38:50 |
| Eccentricity: | 0.0006357 |
| inclination: | 3.8075° |
| perigee height: | 35760 km |
| apogee height: | 35814 km |
| right ascension of ascending node: | 43.2388° |
| argument of perigee: | 34.3757° |
| revolutions per day: | 1.00270446 |
| mean anomaly at epoch: | 21.4207° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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