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 48767U 26145.38495801 +.00000000 +00000-0 +22291-3 0 00000
2 48767 87.8993 263.6298 0001230 107.7928 252.3337 13.16195024 01
| Epoch (UTC): | 25 May 2026 09:14:20 |
| Eccentricity: | 0.0001230 |
| inclination: | 87.8993° |
| perigee height: | 1198 km |
| apogee height: | 1200 km |
| right ascension of ascending node: | 263.6298° |
| argument of perigee: | 107.7928° |
| revolutions per day: | 13.16195024 |
| mean anomaly at epoch: | 252.3337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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