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 00012U 26073.81381654 +.00000000 +00000-0 +29591-3 0 00009
2 00012 32.9031 197.8438 1646632 325.3410 24.9886 11.48568356 03
| Epoch (UTC): | 14 March 2026 19:31:53 |
| Eccentricity: | 0.1646632 |
| inclination: | 32.9031° |
| perigee height: | 553 km |
| apogee height: | 3286 km |
| right ascension of ascending node: | 197.8438° |
| argument of perigee: | 325.3410° |
| revolutions per day: | 11.48568356 |
| mean anomaly at epoch: | 24.9886° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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