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 02834U 26088.00150625 +.00000000 +00000-0 +65408-4 0 00000
2 02834 69.9724 304.7513 0009590 301.4618 58.5549 13.96180902 00
| Epoch (UTC): | 29 March 2026 00:02:10 |
| Eccentricity: | 0.0009590 |
| inclination: | 69.9724° |
| perigee height: | 900 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 304.7513° |
| argument of perigee: | 301.4618° |
| revolutions per day: | 13.96180902 |
| mean anomaly at epoch: | 58.5549° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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