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 60398U 26145.48097017 +.00000000 +00000-0 +11268-4 0 00005
2 60398 53.1603 67.7248 0000995 93.5200 266.5932 15.69710717 09
| Epoch (UTC): | 25 May 2026 11:32:35 |
| Eccentricity: | 0.0000995 |
| inclination: | 53.1603° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 67.7248° |
| argument of perigee: | 93.5200° |
| revolutions per day: | 15.69710717 |
| mean anomaly at epoch: | 266.5932° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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