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 43773U 26050.04745017 +.00000000 +00000-0 +24873-3 0 00005
2 43773 97.4143 96.0731 0011566 43.5113 316.7028 15.12232029 00
| Epoch (UTC): | 19 February 2026 01:08:19 |
| Eccentricity: | 0.0011566 |
| inclination: | 97.4143° |
| perigee height: | 521 km |
| apogee height: | 537 km |
| right ascension of ascending node: | 96.0731° |
| argument of perigee: | 43.5113° |
| revolutions per day: | 15.12232029 |
| mean anomaly at epoch: | 316.7028° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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