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 49260U 26145.46687470 +.00000000 +00000-0 +68833-4 0 00006
2 49260 98.1858 215.9697 0001451 97.7775 262.3589 14.57115814 06
| Epoch (UTC): | 25 May 2026 11:12:17 |
| Eccentricity: | 0.0001451 |
| inclination: | 98.1858° |
| perigee height: | 701 km |
| apogee height: | 704 km |
| right ascension of ascending node: | 215.9697° |
| argument of perigee: | 97.7775° |
| revolutions per day: | 14.57115814 |
| mean anomaly at epoch: | 262.3589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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