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 48768U 26145.37606867 +.00000000 +00000-0 +22905-3 0 00008
2 48768 87.8997 263.7338 0001490 96.0565 264.0735 13.15547687 04
| Epoch (UTC): | 25 May 2026 09:01:32 |
| Eccentricity: | 0.0001490 |
| inclination: | 87.8997° |
| perigee height: | 1201 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7338° |
| argument of perigee: | 96.0565° |
| revolutions per day: | 13.15547687 |
| mean anomaly at epoch: | 264.0735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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