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 37223U 26160.80708435 +.00000000 +00000-0 +25536-3 0 00004
2 37223 71.9705 56.4552 0011649 44.3853 315.8253 15.00308954 05
| Epoch (UTC): | 09 June 2026 19:22:12 |
| Eccentricity: | 0.0011649 |
| inclination: | 71.9705° |
| perigee height: | 558 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 56.4552° |
| argument of perigee: | 44.3853° |
| revolutions per day: | 15.00308954 |
| mean anomaly at epoch: | 315.8253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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