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 69000U 26145.58335647 +.00000000 +00000-0 +53603-2 0 00006
2 69000 97.7396 43.4578 0002424 181.7766 62.5628 14.91656787 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0002424 |
| inclination: | 97.7396° |
| perigee height: | 591 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 43.4578° |
| argument of perigee: | 181.7766° |
| revolutions per day: | 14.91656787 |
| mean anomaly at epoch: | 62.5628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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