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 48778U 26145.55353568 +.00000000 +00000-0 +60159-3 0 00009
2 48778 87.8999 263.7006 0001719 104.5372 255.5949 13.15548308 07
| Epoch (UTC): | 25 May 2026 13:17:05 |
| Eccentricity: | 0.0001719 |
| inclination: | 87.8999° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7006° |
| argument of perigee: | 104.5372° |
| revolutions per day: | 13.15548308 |
| mean anomaly at epoch: | 255.5949° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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