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 57390U 26144.09084323 +.00000000 +00000-0 +13522-2 0 00008
2 57390 99.4444 194.1069 0033888 214.5574 145.3505 16.19263619 05
| Epoch (UTC): | 24 May 2026 02:10:48 |
| Eccentricity: | 0.0033888 |
| inclination: | 99.4444° |
| perigee height: | 199 km |
| apogee height: | 244 km |
| right ascension of ascending node: | 194.1069° |
| argument of perigee: | 214.5574° |
| revolutions per day: | 16.19263619 |
| mean anomaly at epoch: | 145.3505° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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