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 48077U 26144.95000350 +.00000000 +00000-0 +94083-3 0 00005
2 48077 87.8941 324.8511 0001859 95.2190 264.9151 13.13468446 06
| Epoch (UTC): | 24 May 2026 22:48:00 |
| Eccentricity: | 0.0001859 |
| inclination: | 87.8941° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.8511° |
| argument of perigee: | 95.2190° |
| revolutions per day: | 13.13468446 |
| mean anomaly at epoch: | 264.9151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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