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 68653U 26145.21513278 +.00000000 +00000-0 +43181-4 0 00009
2 68653 88.9868 323.3334 0010808 67.2826 292.9476 13.67484062 06
| Epoch (UTC): | 25 May 2026 05:09:47 |
| Eccentricity: | 0.0010808 |
| inclination: | 88.9868° |
| perigee height: | 1001 km |
| apogee height: | 1017 km |
| right ascension of ascending node: | 323.3334° |
| argument of perigee: | 67.2826° |
| revolutions per day: | 13.67484062 |
| mean anomaly at epoch: | 292.9476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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