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 43807U 26155.10196956 +.00000000 +00000-0 +43833-3 0 00005
2 43807 97.4221 211.0707 0004798 1.7762 358.3490 15.20380562 02
| Epoch (UTC): | 04 June 2026 02:26:50 |
| Eccentricity: | 0.0004798 |
| inclination: | 97.4221° |
| perigee height: | 501 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 211.0707° |
| argument of perigee: | 1.7762° |
| revolutions per day: | 15.20380562 |
| mean anomaly at epoch: | 358.3490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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