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 61965U 26145.27231951 +.00000000 +00000-0 +10949-2 0 00003
2 61965 43.0044 100.2883 0001490 264.8018 95.2664 15.27595314 03
| Epoch (UTC): | 25 May 2026 06:32:08 |
| Eccentricity: | 0.0001490 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 100.2883° |
| argument of perigee: | 264.8018° |
| revolutions per day: | 15.27595314 |
| mean anomaly at epoch: | 95.2664° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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