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 48604U 26145.28744786 +.00000000 +00000-0 -17383-4 0 00006
2 48604 53.1605 152.6629 0000936 86.6097 273.5012 15.31704443 01
| Epoch (UTC): | 25 May 2026 06:53:55 |
| Eccentricity: | 0.0000936 |
| inclination: | 53.1605° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 152.6629° |
| argument of perigee: | 86.6097° |
| revolutions per day: | 15.31704443 |
| mean anomaly at epoch: | 273.5012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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