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 68630U 26145.34361080 +.00000000 +00000-0 +22911-3 0 00007
2 68630 60.0218 265.8058 0023746 8.5877 351.5605 15.24399540 00
| Epoch (UTC): | 25 May 2026 08:14:47 |
| Eccentricity: | 0.0023746 |
| inclination: | 60.0218° |
| perigee height: | 476 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 265.8058° |
| argument of perigee: | 8.5877° |
| revolutions per day: | 15.24399540 |
| mean anomaly at epoch: | 351.5605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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