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 40010U 26145.59676470 +.00000000 +00000-0 +10648-3 0 00002
2 40010 97.5428 346.4010 0009734 41.7203 318.4754 14.85440932 02
| Epoch (UTC): | 25 May 2026 14:19:20 |
| Eccentricity: | 0.0009734 |
| inclination: | 97.5428° |
| perigee height: | 605 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 346.4010° |
| argument of perigee: | 41.7203° |
| revolutions per day: | 14.85440932 |
| mean anomaly at epoch: | 318.4754° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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