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 40024U 26108.31696122 +.00000000 +00000-0 +38026-3 0 00002
2 40024 98.0776 135.4770 0004548 56.4057 303.7615 15.29558904 07
| Epoch (UTC): | 18 April 2026 07:36:25 |
| Eccentricity: | 0.0004548 |
| inclination: | 98.0776° |
| perigee height: | 474 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 135.4770° |
| argument of perigee: | 56.4057° |
| revolutions per day: | 15.29558904 |
| mean anomaly at epoch: | 303.7615° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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