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 37389U 26114.23725309 +.00000000 +00000-0 -41033-4 0 00004
2 37389 98.3489 93.8427 0014724 137.3305 222.9022 14.25188510 00
| Epoch (UTC): | 24 April 2026 05:41:38 |
| Eccentricity: | 0.0014724 |
| inclination: | 98.3489° |
| perigee height: | 797 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 93.8427° |
| argument of perigee: | 137.3305° |
| revolutions per day: | 14.25188510 |
| mean anomaly at epoch: | 222.9022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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