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 26104.44896654 +.00000000 +00000-0 +15224-3 0 00004
2 00005 34.2468 151.0106 1836455 211.1218 136.6571 10.85969996 07
| Epoch (UTC): | 14 April 2026 10:46:30 |
| Eccentricity: | 0.1836455 |
| inclination: | 34.2468° |
| perigee height: | 654 km |
| apogee height: | 3817 km |
| right ascension of ascending node: | 151.0106° |
| argument of perigee: | 211.1218° |
| revolutions per day: | 10.85969996 |
| mean anomaly at epoch: | 136.6571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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