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 55034U 26145.13977492 +.00000000 +00000-0 +22558-3 0 00005
2 55034 97.3214 204.2852 0008064 189.0795 171.0303 15.32982376 06
| Epoch (UTC): | 25 May 2026 03:21:16 |
| Eccentricity: | 0.0008064 |
| inclination: | 97.3214° |
| perigee height: | 461 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 204.2852° |
| argument of perigee: | 189.0795° |
| revolutions per day: | 15.32982376 |
| mean anomaly at epoch: | 171.0303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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