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 53197U 26145.12150580 +.00000000 +00000-0 +40865-4 0 00005
2 53197 97.4493 205.0382 0001904 148.2420 211.8922 15.05650210 08
| Epoch (UTC): | 25 May 2026 02:54:58 |
| Eccentricity: | 0.0001904 |
| inclination: | 97.4493° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 205.0382° |
| argument of perigee: | 148.2420° |
| revolutions per day: | 15.05650210 |
| mean anomaly at epoch: | 211.8922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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