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 48462U 26145.40033764 +.00000000 +00000-0 +32275-3 0 00004
2 48462 53.1600 194.2803 0001515 97.7358 262.3815 15.31712392 00
| Epoch (UTC): | 25 May 2026 09:36:29 |
| Eccentricity: | 0.0001515 |
| inclination: | 53.1600° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 194.2803° |
| argument of perigee: | 97.7358° |
| revolutions per day: | 15.31712392 |
| mean anomaly at epoch: | 262.3815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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