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 54376U 26145.40167608 +.00000000 +00000-0 +32124-3 0 00003
2 54376 35.0086 122.8274 0006573 189.7605 170.2983 15.23059236 08
| Epoch (UTC): | 25 May 2026 09:38:24 |
| Eccentricity: | 0.0006573 |
| inclination: | 35.0086° |
| perigee height: | 492 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 122.8274° |
| argument of perigee: | 189.7605° |
| revolutions per day: | 15.23059236 |
| mean anomaly at epoch: | 170.2983° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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