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 54770U 26145.44003411 +.00000000 +00000-0 +12574-3 0 00003
2 54770 53.2119 44.7565 0001444 104.1205 255.9947 15.08832414 00
| Epoch (UTC): | 25 May 2026 10:33:38 |
| Eccentricity: | 0.0001444 |
| inclination: | 53.2119° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 44.7565° |
| argument of perigee: | 104.1205° |
| revolutions per day: | 15.08832414 |
| mean anomaly at epoch: | 255.9947° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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