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 26816U 26087.80904777 +.00000000 +00000-0 +33840-2 0 00001
2 26816 100.3451 30.1844 0060841 326.9234 88.8674 13.57979731 00
| Epoch (UTC): | 28 March 2026 19:25:01 |
| Eccentricity: | 0.0060841 |
| inclination: | 100.3451° |
| perigee height: | 998 km |
| apogee height: | 1088 km |
| right ascension of ascending node: | 30.1844° |
| argument of perigee: | 326.9234° |
| revolutions per day: | 13.57979731 |
| mean anomaly at epoch: | 88.8674° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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