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 00005U 26156.24022257 +.00000000 +00000-0 +45480-3 0 00006
2 00005 34.2474 351.1964 1835477 84.6266 295.9874 10.85992282 07
| Epoch (UTC): | 05 June 2026 05:45:55 |
| Eccentricity: | 0.1835477 |
| inclination: | 34.2474° |
| perigee height: | 654 km |
| apogee height: | 3816 km |
| right ascension of ascending node: | 351.1964° |
| argument of perigee: | 84.6266° |
| revolutions per day: | 10.85992282 |
| mean anomaly at epoch: | 295.9874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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