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 68203U 26145.15067090 +.00000000 +00000-0 +38084-3 0 00004
2 68203 97.5328 220.3603 0011333 32.7429 327.4502 15.11363163 02
| Epoch (UTC): | 25 May 2026 03:36:57 |
| Eccentricity: | 0.0011333 |
| inclination: | 97.5328° |
| perigee height: | 524 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 220.3603° |
| argument of perigee: | 32.7429° |
| revolutions per day: | 15.11363163 |
| mean anomaly at epoch: | 327.4502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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