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 42844U 26103.74259833 +.00000000 +00000-0 +29650-3 0 00003
2 42844 97.3710 279.1295 0003491 228.9646 131.1290 15.23098327 07
| Epoch (UTC): | 13 April 2026 17:49:20 |
| Eccentricity: | 0.0003491 |
| inclination: | 97.3710° |
| perigee height: | 494 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 279.1295° |
| argument of perigee: | 228.9646° |
| revolutions per day: | 15.23098327 |
| mean anomaly at epoch: | 131.1290° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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