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 37793U 26145.19747676 +.00000000 +00000-0 +85891-4 0 00002
2 37793 98.2378 55.2266 0043567 157.8312 359.1148 14.76877777 08
| Epoch (UTC): | 25 May 2026 04:44:21 |
| Eccentricity: | 0.0043567 |
| inclination: | 98.2378° |
| perigee height: | 609 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 55.2266° |
| argument of perigee: | 157.8312° |
| revolutions per day: | 14.76877777 |
| mean anomaly at epoch: | 359.1148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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