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 65803U 26145.56475845 +.00000000 +00000-0 +14063-3 0 00004
2 65803 97.4512 8.2861 0002072 85.9748 274.1716 15.05654412 00
| Epoch (UTC): | 25 May 2026 13:33:15 |
| Eccentricity: | 0.0002072 |
| inclination: | 97.4512° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 8.2861° |
| argument of perigee: | 85.9748° |
| revolutions per day: | 15.05654412 |
| mean anomaly at epoch: | 274.1716° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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