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 37380U 26102.20271450 +.00000000 +00000-0 +79659-4 0 00006
2 37380 71.9707 292.7936 0017209 240.1972 119.7483 14.84534710 06
| Epoch (UTC): | 12 April 2026 04:51:54 |
| Eccentricity: | 0.0017209 |
| inclination: | 71.9707° |
| perigee height: | 603 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 292.7936° |
| argument of perigee: | 240.1972° |
| revolutions per day: | 14.84534710 |
| mean anomaly at epoch: | 119.7483° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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