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 69030U 26145.59163852 +.00000000 +00000-0 +89158-3 0 00002
2 69030 97.2848 0.3660 0001418 99.9491 260.1935 15.75188905 03
| Epoch (UTC): | 25 May 2026 14:11:57 |
| Eccentricity: | 0.0001418 |
| inclination: | 97.2848° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 0.3660° |
| argument of perigee: | 99.9491° |
| revolutions per day: | 15.75188905 |
| mean anomaly at epoch: | 260.1935° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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