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 68853U 26145.29634000 +.00000000 +00000-0 +40561-3 0 00004
2 68853 97.2855 159.9621 0001692 92.8923 267.2522 15.49217212 02
| Epoch (UTC): | 25 May 2026 07:06:43 |
| Eccentricity: | 0.0001692 |
| inclination: | 97.2855° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 159.9621° |
| argument of perigee: | 92.8923° |
| revolutions per day: | 15.49217212 |
| mean anomaly at epoch: | 267.2522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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