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 26072.05676029 +.00000000 +00000-0 +10636-2 0 00000
2 40021 98.0637 118.8819 0005782 75.3847 284.8044 15.50256532 08
| Epoch (UTC): | 13 March 2026 01:21:44 |
| Eccentricity: | 0.0005782 |
| inclination: | 98.0637° |
| perigee height: | 412 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 118.8819° |
| argument of perigee: | 75.3847° |
| revolutions per day: | 15.50256532 |
| mean anomaly at epoch: | 284.8044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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