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 37788U 26162.21751235 +.00000000 +00000-0 +11084-3 0 00006
2 37788 98.2707 59.7165 0035229 138.0951 341.2275 14.76512595 08
| Epoch (UTC): | 11 June 2026 05:13:13 |
| Eccentricity: | 0.0035229 |
| inclination: | 98.2707° |
| perigee height: | 616 km |
| apogee height: | 665 km |
| right ascension of ascending node: | 59.7165° |
| argument of perigee: | 138.0951° |
| revolutions per day: | 14.76512595 |
| mean anomaly at epoch: | 341.2275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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