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 65070U 26145.62666454 +.00000000 +00000-0 +30149-3 0 00008
2 65070 97.4455 222.6310 0002041 166.1007 194.0277 15.05653114 09
| Epoch (UTC): | 25 May 2026 15:02:23 |
| Eccentricity: | 0.0002041 |
| inclination: | 97.4455° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 222.6310° |
| argument of perigee: | 166.1007° |
| revolutions per day: | 15.05653114 |
| mean anomaly at epoch: | 194.0277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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