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 37875U 26145.58407284 +.00000000 +00000-0 +31496-3 0 00005
2 37875 97.1160 185.2189 0008442 313.4401 46.6135 15.26265905 00
| Epoch (UTC): | 25 May 2026 14:01:03 |
| Eccentricity: | 0.0008442 |
| inclination: | 97.1160° |
| perigee height: | 481 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 185.2189° |
| argument of perigee: | 313.4401° |
| revolutions per day: | 15.26265905 |
| mean anomaly at epoch: | 46.6135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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