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 61899U 26145.64952926 +.00000000 +00000-0 +42590-3 0 00000
2 61899 97.4103 217.5523 0008530 107.4582 252.7583 15.14928091 09
| Epoch (UTC): | 25 May 2026 15:35:19 |
| Eccentricity: | 0.0008530 |
| inclination: | 97.4103° |
| perigee height: | 515 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 217.5523° |
| argument of perigee: | 107.4582° |
| revolutions per day: | 15.14928091 |
| mean anomaly at epoch: | 252.7583° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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