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 46457U 26145.61131977 +.00000000 +00000-0 +64829-3 0 00004
2 46457 97.2280 197.7421 0010742 232.8339 127.1938 15.60780293 03
| Epoch (UTC): | 25 May 2026 14:40:18 |
| Eccentricity: | 0.0010742 |
| inclination: | 97.2280° |
| perigee height: | 378 km |
| apogee height: | 393 km |
| right ascension of ascending node: | 197.7421° |
| argument of perigee: | 232.8339° |
| revolutions per day: | 15.60780293 |
| mean anomaly at epoch: | 127.1938° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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