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 48948U 26145.29403887 +.00000000 +00000-0 +38463-3 0 00002
2 48948 97.6812 345.5176 0005815 64.3228 295.8632 15.67482292 04
| Epoch (UTC): | 25 May 2026 07:03:24 |
| Eccentricity: | 0.0005815 |
| inclination: | 97.6812° |
| perigee height: | 362 km |
| apogee height: | 370 km |
| right ascension of ascending node: | 345.5176° |
| argument of perigee: | 64.3228° |
| revolutions per day: | 15.67482292 |
| mean anomaly at epoch: | 295.8632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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