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 48273U 26145.20372403 +.00000000 +00000-0 +15225-2 0 00003
2 48273 97.5654 230.5157 0001792 203.9638 156.1534 15.57983322 05
| Epoch (UTC): | 25 May 2026 04:53:21 |
| Eccentricity: | 0.0001792 |
| inclination: | 97.5654° |
| perigee height: | 392 km |
| apogee height: | 395 km |
| right ascension of ascending node: | 230.5157° |
| argument of perigee: | 203.9638° |
| revolutions per day: | 15.57983322 |
| mean anomaly at epoch: | 156.1534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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