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 26075.85092086 +.00000000 +00000-0 +24323-3 0 00002
2 43773 97.4097 121.1309 0009019 312.9137 47.1337 15.12541279 06
| Epoch (UTC): | 16 March 2026 20:25:19 |
| Eccentricity: | 0.0009019 |
| inclination: | 97.4097° |
| perigee height: | 522 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 121.1309° |
| argument of perigee: | 312.9137° |
| revolutions per day: | 15.12541279 |
| mean anomaly at epoch: | 47.1337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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