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 61246U 26145.13077535 +.00000000 +00000-0 +52948-4 0 00003
2 61246 53.1573 39.3476 0000919 66.2510 293.8604 15.69717120 07
| Epoch (UTC): | 25 May 2026 03:08:18 |
| Eccentricity: | 0.0000919 |
| inclination: | 53.1573° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 39.3476° |
| argument of perigee: | 66.2510° |
| revolutions per day: | 15.69717120 |
| mean anomaly at epoch: | 293.8604° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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