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 37168U 26145.56361487 +.00000000 +00000-0 +16022-3 0 00000
2 37168 97.7364 30.5814 0079603 281.9205 121.6524 15.16376774 04
| Epoch (UTC): | 25 May 2026 13:31:36 |
| Eccentricity: | 0.0079603 |
| inclination: | 97.7364° |
| perigee height: | 462 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 30.5814° |
| argument of perigee: | 281.9205° |
| revolutions per day: | 15.16376774 |
| mean anomaly at epoch: | 121.6524° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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