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 28496U 26150.40001942 +.00000000 +00000-0 +24571-3 0 00008
2 28496 98.2259 86.3871 0001146 11.6057 348.5189 14.96474701 02
| Epoch (UTC): | 30 May 2026 09:36:01 |
| Eccentricity: | 0.0001146 |
| inclination: | 98.2259° |
| perigee height: | 577 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 86.3871° |
| argument of perigee: | 11.6057° |
| revolutions per day: | 14.96474701 |
| mean anomaly at epoch: | 348.5189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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