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 69181U 26145.17824852 +.00000000 +00000-0 +23752-3 0 00005
2 69181 41.4669 101.7926 0110256 128.5701 232.5091 16.01258577 06
| Epoch (UTC): | 25 May 2026 04:16:40 |
| Eccentricity: | 0.0110256 |
| inclination: | 41.4669° |
| perigee height: | 198 km |
| apogee height: | 344 km |
| right ascension of ascending node: | 101.7926° |
| argument of perigee: | 128.5701° |
| revolutions per day: | 16.01258577 |
| mean anomaly at epoch: | 232.5091° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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