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 68623U 26145.58335647 +.00000000 +00000-0 -71833-2 0 00002
2 68623 97.2852 345.1541 0001884 68.6580 216.3429 15.49407740 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001884 |
| inclination: | 97.2852° |
| perigee height: | 417 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 345.1541° |
| argument of perigee: | 68.6580° |
| revolutions per day: | 15.49407740 |
| mean anomaly at epoch: | 216.3429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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