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 16614U 26156.41697608 +.00000000 +00000-0 +13687-2 0 00009
2 16614 98.7966 253.8635 4690982 254.4315 156.5430 5.50601429 05
| Epoch (UTC): | 05 June 2026 10:00:26 |
| Eccentricity: | 0.4690982 |
| inclination: | 98.7966° |
| perigee height: | 814 km |
| apogee height: | 13524 km |
| right ascension of ascending node: | 253.8635° |
| argument of perigee: | 254.4315° |
| revolutions per day: | 5.50601429 |
| mean anomaly at epoch: | 156.5430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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