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 48788U 26145.57174719 +.00000000 +00000-0 +13043-3 0 00001
2 48788 87.9002 263.6856 0002120 91.4826 268.6547 13.15547660 00
| Epoch (UTC): | 25 May 2026 13:43:18 |
| Eccentricity: | 0.0002120 |
| inclination: | 87.9002° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.6856° |
| argument of perigee: | 91.4826° |
| revolutions per day: | 13.15547660 |
| mean anomaly at epoch: | 268.6547° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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