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 68850U 26145.45698120 +.00000000 +00000-0 +12848-2 0 00008
2 68850 97.2841 160.0490 0000423 47.4335 312.6952 15.49246133 01
| Epoch (UTC): | 25 May 2026 10:58:03 |
| Eccentricity: | 0.0000423 |
| inclination: | 97.2841° |
| perigee height: | 419 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 160.0490° |
| argument of perigee: | 47.4335° |
| revolutions per day: | 15.49246133 |
| mean anomaly at epoch: | 312.6952° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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