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 49167U 26145.30435375 +.00000000 +00000-0 +93896-4 0 00007
2 49167 69.9992 101.2772 0003148 269.4644 90.6155 14.98328562 08
| Epoch (UTC): | 25 May 2026 07:18:16 |
| Eccentricity: | 0.0003148 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 101.2772° |
| argument of perigee: | 269.4644° |
| revolutions per day: | 14.98328562 |
| mean anomaly at epoch: | 90.6155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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