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 02866U 26145.07755580 +.00000000 +00000-0 +00000-0 0 00000
2 02866 2.5705 97.0113 0052921 213.5061 284.3127 1.09425424 09
| Epoch (UTC): | 25 May 2026 01:51:40 |
| Eccentricity: | 0.0052921 |
| inclination: | 2.5705° |
| perigee height: | 33191 km |
| apogee height: | 33612 km |
| right ascension of ascending node: | 97.0113° |
| argument of perigee: | 213.5061° |
| revolutions per day: | 1.09425424 |
| mean anomaly at epoch: | 284.3127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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