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 40057U 26109.26162639 +.00000000 +00000-0 +35154-3 0 00003
2 40057 98.2581 10.9362 0008908 104.7773 255.4435 14.97321426 03
| Epoch (UTC): | 19 April 2026 06:16:44 |
| Eccentricity: | 0.0008908 |
| inclination: | 98.2581° |
| perigee height: | 569 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 10.9362° |
| argument of perigee: | 104.7773° |
| revolutions per day: | 14.97321426 |
| mean anomaly at epoch: | 255.4435° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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