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 40021U 26118.63210690 +.00000000 +00000-0 +10064-2 0 00008
2 40021 98.0532 171.1892 0004416 226.3612 133.7275 15.56321645 08
| Epoch (UTC): | 28 April 2026 15:10:14 |
| Eccentricity: | 0.0004416 |
| inclination: | 98.0532° |
| perigee height: | 395 km |
| apogee height: | 401 km |
| right ascension of ascending node: | 171.1892° |
| argument of perigee: | 226.3612° |
| revolutions per day: | 15.56321645 |
| mean anomaly at epoch: | 133.7275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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