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 48321U 26145.29431406 +.00000000 +00000-0 +14943-4 0 00003
2 48321 53.1602 104.7782 0001185 86.5023 273.6114 15.31702700 05
| Epoch (UTC): | 25 May 2026 07:03:48 |
| Eccentricity: | 0.0001185 |
| inclination: | 53.1602° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 104.7782° |
| argument of perigee: | 86.5023° |
| revolutions per day: | 15.31702700 |
| mean anomaly at epoch: | 273.6114° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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