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 62270U 26145.50977301 +.00000000 +00000-0 +17328-2 0 00003
2 62270 42.9987 313.6035 0001750 266.1374 93.9294 15.70914113 09
| Epoch (UTC): | 25 May 2026 12:14:04 |
| Eccentricity: | 0.0001750 |
| inclination: | 42.9987° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 313.6035° |
| argument of perigee: | 266.1374° |
| revolutions per day: | 15.70914113 |
| mean anomaly at epoch: | 93.9294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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