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 48777U 26145.55829084 +.00000000 +00000-0 +31274-3 0 00005
2 48777 87.8991 263.7226 0001565 75.2591 284.8713 13.15548146 02
| Epoch (UTC): | 25 May 2026 13:23:56 |
| Eccentricity: | 0.0001565 |
| inclination: | 87.8991° |
| perigee height: | 1201 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7226° |
| argument of perigee: | 75.2591° |
| revolutions per day: | 13.15548146 |
| mean anomaly at epoch: | 284.8713° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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