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 53370U 26145.73092115 +.00000000 +00000-0 +18213-3 0 00005
2 53370 97.3461 50.3576 0002631 96.8702 263.2835 15.25529604 08
| Epoch (UTC): | 25 May 2026 17:32:31 |
| Eccentricity: | 0.0002631 |
| inclination: | 97.3461° |
| perigee height: | 487 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 50.3576° |
| argument of perigee: | 96.8702° |
| revolutions per day: | 15.25529604 |
| mean anomaly at epoch: | 263.2835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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