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 26145.61935117 +.00000000 +00000-0 +10144-3 0 00007
2 37389 98.3502 123.7202 0015131 52.2448 308.0101 14.25198640 05
| Epoch (UTC): | 25 May 2026 14:51:51 |
| Eccentricity: | 0.0015131 |
| inclination: | 98.3502° |
| perigee height: | 797 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 123.7202° |
| argument of perigee: | 52.2448° |
| revolutions per day: | 14.25198640 |
| mean anomaly at epoch: | 308.0101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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