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 39233U 26145.58884178 +.00000000 +00000-0 +00000-0 0 00000
2 39233 0.0521 8.9938 0002665 49.4286 62.2142 1.00271406 07
| Epoch (UTC): | 25 May 2026 14:07:55 |
| Eccentricity: | 0.0002665 |
| inclination: | 0.0521° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 8.9938° |
| argument of perigee: | 49.4286° |
| revolutions per day: | 1.00271406 |
| mean anomaly at epoch: | 62.2142° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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