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 61010U 26145.50938006 +.00000000 +00000-0 +12548-3 0 00003
2 61010 53.1606 68.6396 0001305 98.1157 261.9992 15.30172294 01
| Epoch (UTC): | 25 May 2026 12:13:30 |
| Eccentricity: | 0.0001305 |
| inclination: | 53.1606° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 68.6396° |
| argument of perigee: | 98.1157° |
| revolutions per day: | 15.30172294 |
| mean anomaly at epoch: | 261.9992° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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