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 26032.04858778 +.00000000 +00000-0 +52830-4 0 00002
2 02834 69.9718 64.5573 0006650 2.0268 358.0863 13.96171514 05
| Epoch (UTC): | 01 February 2026 01:09:57 |
| Eccentricity: | 0.0006650 |
| inclination: | 69.9718° |
| perigee height: | 902 km |
| apogee height: | 912 km |
| right ascension of ascending node: | 64.5573° |
| argument of perigee: | 2.0268° |
| revolutions per day: | 13.96171514 |
| mean anomaly at epoch: | 358.0863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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