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 07493U 26088.17298007 +.00000000 +00000-0 +62124-4 0 00003
2 07493 81.1593 262.3191 0083902 64.3295 296.6510 14.08031317 04
| Epoch (UTC): | 29 March 2026 04:09:05 |
| Eccentricity: | 0.0083902 |
| inclination: | 81.1593° |
| perigee height: | 805 km |
| apogee height: | 927 km |
| right ascension of ascending node: | 262.3191° |
| argument of perigee: | 64.3295° |
| revolutions per day: | 14.08031317 |
| mean anomaly at epoch: | 296.6510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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