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 48468U 26145.51224286 +.00000000 +00000-0 +40329-4 0 00003
2 48468 53.1586 194.0641 0001246 97.9607 262.1536 15.31698944 01
| Epoch (UTC): | 25 May 2026 12:17:37 |
| Eccentricity: | 0.0001246 |
| inclination: | 53.1586° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 194.0641° |
| argument of perigee: | 97.9607° |
| revolutions per day: | 15.31698944 |
| mean anomaly at epoch: | 262.1536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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