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 37622U 26087.07169343 +.00000000 +00000-0 +52921-3 0 00001
2 37622 98.3106 124.7333 0032019 213.4549 174.8396 14.48062835 04
| Epoch (UTC): | 28 March 2026 01:43:14 |
| Eccentricity: | 0.0032019 |
| inclination: | 98.3106° |
| perigee height: | 709 km |
| apogee height: | 755 km |
| right ascension of ascending node: | 124.7333° |
| argument of perigee: | 213.4549° |
| revolutions per day: | 14.48062835 |
| mean anomaly at epoch: | 174.8396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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