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 49125U 26145.46124022 +.00000000 +00000-0 +00000-0 0 00003
2 49125 0.0143 277.6983 0001743 158.5532 74.2468 1.00273060 07
| Epoch (UTC): | 25 May 2026 11:04:11 |
| Eccentricity: | 0.0001743 |
| inclination: | 0.0143° |
| perigee height: | 35779 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 277.6983° |
| argument of perigee: | 158.5532° |
| revolutions per day: | 1.00273060 |
| mean anomaly at epoch: | 74.2468° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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