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 68465U 26145.62333909 +.00000000 +00000-0 +15387-3 0 00002
2 68465 97.4512 104.3485 0004520 129.9584 230.2047 15.17389372 07
| Epoch (UTC): | 25 May 2026 14:57:36 |
| Eccentricity: | 0.0004520 |
| inclination: | 97.4512° |
| perigee height: | 511 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 104.3485° |
| argument of perigee: | 129.9584° |
| revolutions per day: | 15.17389372 |
| mean anomaly at epoch: | 230.2047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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