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 26140.61134186 +.00000000 +00000-0 +56106-4 0 00009
2 37380 71.9715 207.0400 0014988 172.1757 187.9645 14.84594994 03
| Epoch (UTC): | 20 May 2026 14:40:19 |
| Eccentricity: | 0.0014988 |
| inclination: | 71.9715° |
| perigee height: | 604 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 207.0400° |
| argument of perigee: | 172.1757° |
| revolutions per day: | 14.84594994 |
| mean anomaly at epoch: | 187.9645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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