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 28395U 26128.17398367 +.00000000 +00000-0 +79489-3 0 00003
2 28395 49.4151 115.4723 5138419 43.5949 347.1629 5.38910352 09
| Epoch (UTC): | 08 May 2026 04:10:32 |
| Eccentricity: | 0.5138419 |
| inclination: | 49.4151° |
| perigee height: | 303 km |
| apogee height: | 14425 km |
| right ascension of ascending node: | 115.4723° |
| argument of perigee: | 43.5949° |
| revolutions per day: | 5.38910352 |
| mean anomaly at epoch: | 347.1629° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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