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 26042.19632580 +.00000000 +00000-0 +85913-4 0 00004
2 07493 81.1628 307.3529 0080776 193.1778 166.7283 14.08015674 03
| Epoch (UTC): | 11 February 2026 04:42:42 |
| Eccentricity: | 0.0080776 |
| inclination: | 81.1628° |
| perigee height: | 808 km |
| apogee height: | 925 km |
| right ascension of ascending node: | 307.3529° |
| argument of perigee: | 193.1778° |
| revolutions per day: | 14.08015674 |
| mean anomaly at epoch: | 166.7283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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