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 68023U 26145.37556574 +.00000000 +00000-0 +66704-3 0 00008
2 68023 97.2843 94.3644 0001778 104.1760 255.9680 15.33447142 05
| Epoch (UTC): | 25 May 2026 09:00:48 |
| Eccentricity: | 0.0001778 |
| inclination: | 97.2843° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 94.3644° |
| argument of perigee: | 104.1760° |
| revolutions per day: | 15.33447142 |
| mean anomaly at epoch: | 255.9680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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