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 26145.39515911 +.00000000 +00000-0 +75357-4 0 00002
2 37790 97.8536 130.7248 0013422 50.9387 309.3006 14.60846701 03
| Epoch (UTC): | 25 May 2026 09:29:01 |
| Eccentricity: | 0.0013422 |
| inclination: | 97.8536° |
| perigee height: | 681 km |
| apogee height: | 700 km |
| right ascension of ascending node: | 130.7248° |
| argument of perigee: | 50.9387° |
| revolutions per day: | 14.60846701 |
| mean anomaly at epoch: | 309.3006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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