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 68303U 26145.32407669 +.00000000 +00000-0 +93495-3 0 00001
2 68303 97.2844 271.6505 0000939 73.6014 286.5355 15.75202743 04
| Epoch (UTC): | 25 May 2026 07:46:40 |
| Eccentricity: | 0.0000939 |
| inclination: | 97.2844° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 271.6505° |
| argument of perigee: | 73.6014° |
| revolutions per day: | 15.75202743 |
| mean anomaly at epoch: | 286.5355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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