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 24277U 26067.71350856 +.00000000 +00000-0 +75655-4 0 00003
2 24277 98.8137 120.8859 0002081 68.1049 292.0354 14.30368107 00
| Epoch (UTC): | 08 March 2026 17:07:27 |
| Eccentricity: | 0.0002081 |
| inclination: | 98.8137° |
| perigee height: | 789 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 120.8859° |
| argument of perigee: | 68.1049° |
| revolutions per day: | 14.30368107 |
| mean anomaly at epoch: | 292.0354° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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