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 37790U 26150.46373716 +.00000000 +00000-0 +10712-3 0 00004
2 37790 97.8537 135.5346 0013119 36.2261 323.9827 14.60851965 08
| Epoch (UTC): | 30 May 2026 11:07:46 |
| Eccentricity: | 0.0013119 |
| inclination: | 97.8537° |
| perigee height: | 681 km |
| apogee height: | 700 km |
| right ascension of ascending node: | 135.5346° |
| argument of perigee: | 36.2261° |
| revolutions per day: | 14.60851965 |
| mean anomaly at epoch: | 323.9827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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