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 61968U 26145.26204009 +.00000000 +00000-0 +63670-3 0 00009
2 61968 43.0026 100.2138 0001521 258.5778 101.4903 15.27590219 02
| Epoch (UTC): | 25 May 2026 06:17:20 |
| Eccentricity: | 0.0001521 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.2138° |
| argument of perigee: | 258.5778° |
| revolutions per day: | 15.27590219 |
| mean anomaly at epoch: | 101.4903° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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