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 37673U 26107.31713836 +.00000000 +00000-0 +79555-4 0 00002
2 37673 97.9803 121.7627 0001118 70.6537 300.1721 14.78531909 00
| Epoch (UTC): | 17 April 2026 07:36:40 |
| Eccentricity: | 0.0001118 |
| inclination: | 97.9803° |
| perigee height: | 633 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 121.7627° |
| argument of perigee: | 70.6537° |
| revolutions per day: | 14.78531909 |
| mean anomaly at epoch: | 300.1721° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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