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 48217U 26145.40391212 +.00000000 +00000-0 +83755-3 0 00006
2 48217 87.8946 294.2409 0001565 106.1451 253.9851 13.14502241 07
| Epoch (UTC): | 25 May 2026 09:41:38 |
| Eccentricity: | 0.0001565 |
| inclination: | 87.8946° |
| perigee height: | 1205 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2409° |
| argument of perigee: | 106.1451° |
| revolutions per day: | 13.14502241 |
| mean anomaly at epoch: | 253.9851° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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