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 26140.56186553 +.00000000 +00000-0 +11723-3 0 00007
2 37168 97.7362 25.4816 0079838 299.5046 177.2704 15.16346593 08
| Epoch (UTC): | 20 May 2026 13:29:05 |
| Eccentricity: | 0.0079838 |
| inclination: | 97.7362° |
| perigee height: | 462 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 25.4816° |
| argument of perigee: | 299.5046° |
| revolutions per day: | 15.16346593 |
| mean anomaly at epoch: | 177.2704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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