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 01208U 26088.04034544 +.00000000 +00000-0 +70531-4 0 00002
2 01208 70.0822 354.8065 0021004 198.2115 178.6650 13.96067368 09
| Epoch (UTC): | 29 March 2026 00:58:05 |
| Eccentricity: | 0.0021004 |
| inclination: | 70.0822° |
| perigee height: | 892 km |
| apogee height: | 923 km |
| right ascension of ascending node: | 354.8065° |
| argument of perigee: | 198.2115° |
| revolutions per day: | 13.96067368 |
| mean anomaly at epoch: | 178.6650° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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