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 68423U 26145.58377057 +.00000000 +00000-0 +23756-3 0 00002
2 68423 97.4489 104.3851 0002108 70.0842 290.0620 15.18613246 06
| Epoch (UTC): | 25 May 2026 14:00:37 |
| Eccentricity: | 0.0002108 |
| inclination: | 97.4489° |
| perigee height: | 509 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 104.3851° |
| argument of perigee: | 70.0842° |
| revolutions per day: | 15.18613246 |
| mean anomaly at epoch: | 290.0620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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