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 68349U 26144.99603536 +.00000000 +00000-0 +62703-3 0 00002
2 68349 53.1584 353.4551 0000497 325.2502 34.8466 15.30210043 03
| Epoch (UTC): | 24 May 2026 23:54:17 |
| Eccentricity: | 0.0000497 |
| inclination: | 53.1584° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 353.4551° |
| argument of perigee: | 325.2502° |
| revolutions per day: | 15.30210043 |
| mean anomaly at epoch: | 34.8466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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