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 48808U 26145.60450611 +.00000000 +00000-0 +00000-0 0 00002
2 48808 0.0997 73.7113 0005333 289.3396 202.5099 1.00271258 04
| Epoch (UTC): | 25 May 2026 14:30:29 |
| Eccentricity: | 0.0005333 |
| inclination: | 0.0997° |
| perigee height: | 35764 km |
| apogee height: | 35809 km |
| right ascension of ascending node: | 73.7113° |
| argument of perigee: | 289.3396° |
| revolutions per day: | 1.00271258 |
| mean anomaly at epoch: | 202.5099° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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