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 68902U 26145.50466851 +.00000000 +00000-0 +69803-3 0 00000
2 68902 97.2856 341.2479 0001686 96.5259 263.6184 15.49226543 02
| Epoch (UTC): | 25 May 2026 12:06:43 |
| Eccentricity: | 0.0001686 |
| inclination: | 97.2856° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 341.2479° |
| argument of perigee: | 96.5259° |
| revolutions per day: | 15.49226543 |
| mean anomaly at epoch: | 263.6184° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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