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 61006U 26145.50620795 +.00000000 +00000-0 +98137-5 0 00001
2 61006 53.1608 68.6229 0001435 93.0415 267.0750 15.30191006 09
| Epoch (UTC): | 25 May 2026 12:08:56 |
| Eccentricity: | 0.0001435 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 68.6229° |
| argument of perigee: | 93.0415° |
| revolutions per day: | 15.30191006 |
| mean anomaly at epoch: | 267.0750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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