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 28414U 26064.79658293 +.00000000 +00000-0 +16312-3 0 00005
2 28414 97.6135 84.0017 0005892 123.9730 236.2057 15.05612405 05
| Epoch (UTC): | 05 March 2026 19:07:04 |
| Eccentricity: | 0.0005892 |
| inclination: | 97.6135° |
| perigee height: | 546 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 84.0017° |
| argument of perigee: | 123.9730° |
| revolutions per day: | 15.05612405 |
| mean anomaly at epoch: | 236.2057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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