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 67606U 26145.15156603 +.00000000 +00000-0 +10201-2 0 00009
2 67606 97.2845 210.3021 0000583 63.4563 296.6739 15.33482268 08
| Epoch (UTC): | 25 May 2026 03:38:15 |
| Eccentricity: | 0.0000583 |
| inclination: | 97.2845° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 210.3021° |
| argument of perigee: | 63.4563° |
| revolutions per day: | 15.33482268 |
| mean anomaly at epoch: | 296.6739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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