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 37224U 26161.09730416 +.00000000 +00000-0 +20922-3 0 00005
2 37224 71.9705 96.3982 0012402 78.5895 281.6668 14.93714221 08
| Epoch (UTC): | 10 June 2026 02:20:07 |
| Eccentricity: | 0.0012402 |
| inclination: | 71.9705° |
| perigee height: | 578 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 96.3982° |
| argument of perigee: | 78.5895° |
| revolutions per day: | 14.93714221 |
| mean anomaly at epoch: | 281.6668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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