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 37781U 26150.49610999 +.00000000 +00000-0 +51004-4 0 00004
2 37781 99.3390 153.5589 0006634 126.1472 234.0292 13.74733174 01
| Epoch (UTC): | 30 May 2026 11:54:23 |
| Eccentricity: | 0.0006634 |
| inclination: | 99.3390° |
| perigee height: | 978 km |
| apogee height: | 988 km |
| right ascension of ascending node: | 153.5589° |
| argument of perigee: | 126.1472° |
| revolutions per day: | 13.74733174 |
| mean anomaly at epoch: | 234.0292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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