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 26093U 26068.84618830 +.00000000 +00000-0 +84287-3 0 00005
2 26093 100.1763 192.9063 0024393 150.7886 209.4680 14.64640890 07
| Epoch (UTC): | 09 March 2026 20:18:30 |
| Eccentricity: | 0.0024393 |
| inclination: | 100.1763° |
| perigee height: | 661 km |
| apogee height: | 695 km |
| right ascension of ascending node: | 192.9063° |
| argument of perigee: | 150.7886° |
| revolutions per day: | 14.64640890 |
| mean anomaly at epoch: | 209.4680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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