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 26073.67032461 +.00000000 +00000-0 +14522-2 0 00003
2 40021 98.0633 120.6867 0005627 70.3630 289.8226 15.50487868 06
| Epoch (UTC): | 14 March 2026 16:05:16 |
| Eccentricity: | 0.0005627 |
| inclination: | 98.0633° |
| perigee height: | 411 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 120.6867° |
| argument of perigee: | 70.3630° |
| revolutions per day: | 15.50487868 |
| mean anomaly at epoch: | 289.8226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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