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 48233U 26145.36584934 +.00000000 +00000-0 -52976-3 0 00006
2 48233 87.8944 294.2617 0001526 103.9940 256.1360 13.14501649 00
| Epoch (UTC): | 25 May 2026 08:46:49 |
| Eccentricity: | 0.0001526 |
| inclination: | 87.8944° |
| perigee height: | 1205 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2617° |
| argument of perigee: | 103.9940° |
| revolutions per day: | 13.14501649 |
| mean anomaly at epoch: | 256.1360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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