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 37153U 26106.22237976 +.00000000 +00000-0 +25085-3 0 00008
2 37153 82.4530 117.0255 0006826 210.0665 150.0023 12.40790897 04
| Epoch (UTC): | 16 April 2026 05:20:13 |
| Eccentricity: | 0.0006826 |
| inclination: | 82.4530° |
| perigee height: | 1498 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 117.0255° |
| argument of perigee: | 210.0665° |
| revolutions per day: | 12.40790897 |
| mean anomaly at epoch: | 150.0023° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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