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 00016U 26049.01445661 +.00000000 +00000-0 +60107-4 0 00006
2 00016 34.2686 289.6660 2021323 337.2610 14.9510 10.49577377 00
| Epoch (UTC): | 18 February 2026 00:20:49 |
| Eccentricity: | 0.2021323 |
| inclination: | 34.2686° |
| perigee height: | 652 km |
| apogee height: | 4215 km |
| right ascension of ascending node: | 289.6660° |
| argument of perigee: | 337.2610° |
| revolutions per day: | 10.49577377 |
| mean anomaly at epoch: | 14.9510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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