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 68316U 26145.35478150 +.00000000 +00000-0 +10213-2 0 00007
2 68316 97.2844 271.6070 0001600 68.8966 291.2470 15.75240786 03
| Epoch (UTC): | 25 May 2026 08:30:53 |
| Eccentricity: | 0.0001600 |
| inclination: | 97.2844° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 271.6070° |
| argument of perigee: | 68.8966° |
| revolutions per day: | 15.75240786 |
| mean anomaly at epoch: | 291.2470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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