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 68698U 26139.53940167 +.00000000 +00000-0 +23163-3 0 00004
2 68698 97.6650 215.1871 0016160 159.8385 200.3486 15.09880071 02
| Epoch (UTC): | 19 May 2026 12:56:44 |
| Eccentricity: | 0.0016160 |
| inclination: | 97.6650° |
| perigee height: | 525 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 215.1871° |
| argument of perigee: | 159.8385° |
| revolutions per day: | 15.09880071 |
| mean anomaly at epoch: | 200.3486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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