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 26074.71838789 +.00000000 +00000-0 -35263-4 0 00004
2 00016 34.2590 215.3171 2020291 85.8250 296.9120 10.49580628 08
| Epoch (UTC): | 15 March 2026 17:14:28 |
| Eccentricity: | 0.2020291 |
| inclination: | 34.2590° |
| perigee height: | 653 km |
| apogee height: | 4214 km |
| right ascension of ascending node: | 215.3171° |
| argument of perigee: | 85.8250° |
| revolutions per day: | 10.49580628 |
| mean anomaly at epoch: | 296.9120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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