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 48010U 26145.51467678 +.00000000 +00000-0 +83050-4 0 00008
2 48010 53.1619 335.3537 0002204 91.7044 268.4210 15.31702271 04
| Epoch (UTC): | 25 May 2026 12:21:08 |
| Eccentricity: | 0.0002204 |
| inclination: | 53.1619° |
| perigee height: | 469 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 335.3537° |
| argument of perigee: | 91.7044° |
| revolutions per day: | 15.31702271 |
| mean anomaly at epoch: | 268.4210° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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