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 26150.50108566 +.00000000 +00000-0 +53909-3 0 00007
2 37875 97.1155 189.9026 0008054 291.7921 68.2461 15.26353081 04
| Epoch (UTC): | 30 May 2026 12:01:33 |
| Eccentricity: | 0.0008054 |
| inclination: | 97.1155° |
| perigee height: | 481 km |
| apogee height: | 492 km |
| right ascension of ascending node: | 189.9026° |
| argument of perigee: | 291.7921° |
| revolutions per day: | 15.26353081 |
| mean anomaly at epoch: | 68.2461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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