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 69024U 26145.65392565 +.00000000 +00000-0 +23469-3 0 00000
2 69024 97.4092 43.8788 0005048 82.7728 277.4081 15.19824691 08
| Epoch (UTC): | 25 May 2026 15:41:39 |
| Eccentricity: | 0.0005048 |
| inclination: | 97.4092° |
| perigee height: | 503 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 43.8788° |
| argument of perigee: | 82.7728° |
| revolutions per day: | 15.19824691 |
| mean anomaly at epoch: | 277.4081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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