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 48673U 26145.33230093 +.00000000 +00000-0 -81656-5 0 00004
2 48673 53.1577 117.9261 0001097 86.1023 274.0102 15.29350615 05
| Epoch (UTC): | 25 May 2026 07:58:30 |
| Eccentricity: | 0.0001097 |
| inclination: | 53.1577° |
| perigee height: | 477 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 117.9261° |
| argument of perigee: | 86.1023° |
| revolutions per day: | 15.29350615 |
| mean anomaly at epoch: | 274.0102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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