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 48062U 26145.41384938 +.00000000 +00000-0 +92721-3 0 00005
2 48062 87.8951 324.7496 0001607 97.9456 262.1855 13.13469402 01
| Epoch (UTC): | 25 May 2026 09:55:56 |
| Eccentricity: | 0.0001607 |
| inclination: | 87.8951° |
| perigee height: | 1209 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7496° |
| argument of perigee: | 97.9456° |
| revolutions per day: | 13.13469402 |
| mean anomaly at epoch: | 262.1855° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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