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 48773U 26145.29208388 +.00000000 +00000-0 -62744-4 0 00008
2 48773 87.8986 263.7689 0001471 102.1542 257.9754 13.15547075 03
| Epoch (UTC): | 25 May 2026 07:00:36 |
| Eccentricity: | 0.0001471 |
| inclination: | 87.8986° |
| perigee height: | 1201 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7689° |
| argument of perigee: | 102.1542° |
| revolutions per day: | 13.15547075 |
| mean anomaly at epoch: | 257.9754° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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