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 39210U 26145.58670564 +.00000000 +00000-0 +89097-4 0 00004
2 39210 98.1039 148.6815 0005333 208.3017 151.7901 14.71468315 09
| Epoch (UTC): | 25 May 2026 14:04:51 |
| Eccentricity: | 0.0005333 |
| inclination: | 98.1039° |
| perigee height: | 653 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 148.6815° |
| argument of perigee: | 208.3017° |
| revolutions per day: | 14.71468315 |
| mean anomaly at epoch: | 151.7901° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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