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 48059U 26145.49679243 +.00000000 +00000-0 +65470-3 0 00006
2 48059 87.8942 324.7510 0002205 103.5125 256.6250 13.13468029 07
| Epoch (UTC): | 25 May 2026 11:55:22 |
| Eccentricity: | 0.0002205 |
| inclination: | 87.8942° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7510° |
| argument of perigee: | 103.5125° |
| revolutions per day: | 13.13468029 |
| mean anomaly at epoch: | 256.6250° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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