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 48478U 26145.39105400 +.00000000 +00000-0 -35504-4 0 00006
2 48478 53.1586 194.3944 0001229 80.9363 279.1777 15.31681180 02
| Epoch (UTC): | 25 May 2026 09:23:07 |
| Eccentricity: | 0.0001229 |
| inclination: | 53.1586° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 194.3944° |
| argument of perigee: | 80.9363° |
| revolutions per day: | 15.31681180 |
| mean anomaly at epoch: | 279.1777° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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