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 02828U 26133.45817821 +.00000000 +00000-0 +77218-4 0 00003
2 02828 69.9688 137.5382 0009731 227.8624 132.1657 13.98080418 05
| Epoch (UTC): | 13 May 2026 10:59:46 |
| Eccentricity: | 0.0009731 |
| inclination: | 69.9688° |
| perigee height: | 893 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 137.5382° |
| argument of perigee: | 227.8624° |
| revolutions per day: | 13.98080418 |
| mean anomaly at epoch: | 132.1657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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