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 65943U 26072.31297397 +.00000000 +00000-0 +11129-2 0 00004
2 65943 51.6233 38.5579 0005696 99.5179 260.6467 15.81842071 00
| Epoch (UTC): | 13 March 2026 07:30:40 |
| Eccentricity: | 0.0005696 |
| inclination: | 51.6233° |
| perigee height: | 321 km |
| apogee height: | 329 km |
| right ascension of ascending node: | 38.5579° |
| argument of perigee: | 99.5179° |
| revolutions per day: | 15.81842071 |
| mean anomaly at epoch: | 260.6467° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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