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 26374U 26150.02343640 +.00000000 +00000-0 +13008-2 0 00005
2 26374 68.9155 25.3192 0429985 80.2213 284.7184 14.60703628 04
| Epoch (UTC): | 30 May 2026 00:33:44 |
| Eccentricity: | 0.0429985 |
| inclination: | 68.9155° |
| perigee height: | 387 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 25.3192° |
| argument of perigee: | 80.2213° |
| revolutions per day: | 14.60703628 |
| mean anomaly at epoch: | 284.7184° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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