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 26071.60492272 +.00000000 +00000-0 +10946-2 0 00000
2 40021 98.0637 118.3770 0005916 76.4423 283.7485 15.50196754 06
| Epoch (UTC): | 12 March 2026 14:31:05 |
| Eccentricity: | 0.0005916 |
| inclination: | 98.0637° |
| perigee height: | 412 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 118.3770° |
| argument of perigee: | 76.4423° |
| revolutions per day: | 15.50196754 |
| mean anomaly at epoch: | 283.7485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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