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 48272U 26145.60624906 +.00000000 +00000-0 +42059-3 0 00000
2 48272 97.5329 203.4212 0008207 33.5041 326.6704 15.05049781 05
| Epoch (UTC): | 25 May 2026 14:32:59 |
| Eccentricity: | 0.0008207 |
| inclination: | 97.5329° |
| perigee height: | 546 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 203.4212° |
| argument of perigee: | 33.5041° |
| revolutions per day: | 15.05049781 |
| mean anomaly at epoch: | 326.6704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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