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 43804U 26145.41880924 +.00000000 +00000-0 +45958-3 0 00000
2 43804 97.4205 205.9049 0009741 11.3025 348.8432 15.27809501 00
| Epoch (UTC): | 25 May 2026 10:03:05 |
| Eccentricity: | 0.0009741 |
| inclination: | 97.4205° |
| perigee height: | 476 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 205.9049° |
| argument of perigee: | 11.3025° |
| revolutions per day: | 15.27809501 |
| mean anomaly at epoch: | 348.8432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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