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 68472U 26144.80647266 +.00000000 +00000-0 +16289-3 0 00005
2 68472 97.7620 103.3663 0005702 107.7102 252.4739 14.90781040 00
| Epoch (UTC): | 24 May 2026 19:21:19 |
| Eccentricity: | 0.0005702 |
| inclination: | 97.7620° |
| perigee height: | 592 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 103.3663° |
| argument of perigee: | 107.7102° |
| revolutions per day: | 14.90781040 |
| mean anomaly at epoch: | 252.4739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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