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 28359U 26070.24459810 +.00000000 +00000-0 +80528-3 0 00004
2 28359 49.5294 22.3172 4500190 130.1471 278.9711 6.50638460 08
| Epoch (UTC): | 11 March 2026 05:52:13 |
| Eccentricity: | 0.4500190 |
| inclination: | 49.5294° |
| perigee height: | 288 km |
| apogee height: | 11196 km |
| right ascension of ascending node: | 22.3172° |
| argument of perigee: | 130.1471° |
| revolutions per day: | 6.50638460 |
| mean anomaly at epoch: | 278.9711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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