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 07298U 26053.75795676 +.00000000 +00000-0 +00000-0 0 00007
2 07298 4.4273 250.5758 0017465 70.7718 244.8058 0.98614764 09
| Epoch (UTC): | 22 February 2026 18:11:27 |
| Eccentricity: | 0.0017465 |
| inclination: | 4.4273° |
| perigee height: | 36183 km |
| apogee height: | 36332 km |
| right ascension of ascending node: | 250.5758° |
| argument of perigee: | 70.7718° |
| revolutions per day: | 0.98614764 |
| mean anomaly at epoch: | 244.8058° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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