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 49295U 26145.36111730 +.00000000 +00000-0 -16173-3 0 00004
2 49295 87.9150 309.5252 0001800 91.1538 268.9801 13.19725669 06
| Epoch (UTC): | 25 May 2026 08:40:00 |
| Eccentricity: | 0.0001800 |
| inclination: | 87.9150° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5252° |
| argument of perigee: | 91.1538° |
| revolutions per day: | 13.19725669 |
| mean anomaly at epoch: | 268.9801° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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