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 43768U 26145.57123889 +.00000000 +00000-0 +26088-3 0 00009
2 43768 97.4311 194.1026 0005318 37.1389 323.0210 15.15177598 06
| Epoch (UTC): | 25 May 2026 13:42:35 |
| Eccentricity: | 0.0005318 |
| inclination: | 97.4311° |
| perigee height: | 517 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 194.1026° |
| argument of perigee: | 37.1389° |
| revolutions per day: | 15.15177598 |
| mean anomaly at epoch: | 323.0210° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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