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 53448U 26145.58636352 +.00000000 +00000-0 +67381-3 0 00001
2 53448 97.5547 274.5555 0002860 107.2451 252.9122 15.65884515 03
| Epoch (UTC): | 25 May 2026 14:04:21 |
| Eccentricity: | 0.0002860 |
| inclination: | 97.5547° |
| perigee height: | 369 km |
| apogee height: | 373 km |
| right ascension of ascending node: | 274.5555° |
| argument of perigee: | 107.2451° |
| revolutions per day: | 15.65884515 |
| mean anomaly at epoch: | 252.9122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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