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 26069.08723611 +.00000000 +00000-0 +11635-2 0 00009
2 40021 98.0632 115.5609 0006054 84.4960 275.6980 15.49868777 09
| Epoch (UTC): | 10 March 2026 02:05:37 |
| Eccentricity: | 0.0006054 |
| inclination: | 98.0632° |
| perigee height: | 413 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 115.5609° |
| argument of perigee: | 84.4960° |
| revolutions per day: | 15.49868777 |
| mean anomaly at epoch: | 275.6980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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