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 67270U 26145.45179225 +.00000000 +00000-0 +38254-3 0 00003
2 67270 97.3946 220.4984 0016134 86.2364 274.0717 15.22964351 01
| Epoch (UTC): | 25 May 2026 10:50:34 |
| Eccentricity: | 0.0016134 |
| inclination: | 97.3946° |
| perigee height: | 486 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 220.4984° |
| argument of perigee: | 86.2364° |
| revolutions per day: | 15.22964351 |
| mean anomaly at epoch: | 274.0717° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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