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 68212U 26145.60571377 +.00000000 +00000-0 +70698-3 0 00009
2 68212 97.2867 21.0184 0002160 85.4292 274.7197 15.33453428 00
| Epoch (UTC): | 25 May 2026 14:32:13 |
| Eccentricity: | 0.0002160 |
| inclination: | 97.2867° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 21.0184° |
| argument of perigee: | 85.4292° |
| revolutions per day: | 15.33453428 |
| mean anomaly at epoch: | 274.7197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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