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 48360U 26145.32503251 +.00000000 +00000-0 +24815-4 0 00007
2 48360 53.1617 1.7180 0001294 92.0288 268.0862 15.31697968 05
| Epoch (UTC): | 25 May 2026 07:48:02 |
| Eccentricity: | 0.0001294 |
| inclination: | 53.1617° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 1.7180° |
| argument of perigee: | 92.0288° |
| revolutions per day: | 15.31697968 |
| mean anomaly at epoch: | 268.0862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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