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 40073U 26088.13876860 +.00000000 +00000-0 +65275-4 0 00009
2 40073 98.3651 35.1479 0005080 195.4254 164.6804 14.82979822 01
| Epoch (UTC): | 29 March 2026 03:19:49 |
| Eccentricity: | 0.0005080 |
| inclination: | 98.3651° |
| perigee height: | 616 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 35.1479° |
| argument of perigee: | 195.4254° |
| revolutions per day: | 14.82979822 |
| mean anomaly at epoch: | 164.6804° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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