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 65279U 26145.41025574 +.00000000 +00000-0 +41103-3 0 00000
2 65279 97.4494 197.8897 0002099 117.1755 242.9687 15.05659286 09
| Epoch (UTC): | 25 May 2026 09:50:46 |
| Eccentricity: | 0.0002099 |
| inclination: | 97.4494° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 197.8897° |
| argument of perigee: | 117.1755° |
| revolutions per day: | 15.05659286 |
| mean anomaly at epoch: | 242.9687° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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