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 48464U 26145.55448241 +.00000000 +00000-0 -31785-3 0 00008
2 48464 53.1581 193.6826 0001059 88.2521 271.8601 15.31695429 07
| Epoch (UTC): | 25 May 2026 13:18:27 |
| Eccentricity: | 0.0001059 |
| inclination: | 53.1581° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 193.6826° |
| argument of perigee: | 88.2521° |
| revolutions per day: | 15.31695429 |
| mean anomaly at epoch: | 271.8601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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