▸Orbital parameters

Orbit class	SSO
Inclination	97.4125°
Eccentricity	0.0002533
Period	94.0 min
Apogee	473 km
Perigee	469 km
Mean motion	15.31666642 rev/day
RAAN	263.1027°
Arg of perigee	350.0703°
Mean anomaly	10.0488°
B*	1.4303e-4
Rev at epoch	3,357

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 66667U 25276B 26188.14120904 .00004295 00000-0 14303-3 0 9993

2 66667 97.4125 263.1027 0002533 350.0703 10.0488 15.31666642 33572

▸ source OMM (JSON)

{
  "OBJECT_NAME": "PELICAN-5",
  "OBJECT_ID": "2025-276B",
  "EPOCH": "2026-07-07T03:23:20.461+00:00",
  "MEAN_MOTION": 15.31666642,
  "ECCENTRICITY": 0.0002533,
  "INCLINATION": 97.4125,
  "RA_OF_ASC_NODE": 263.1027,
  "ARG_OF_PERICENTER": 350.0703,
  "MEAN_ANOMALY": 10.0488,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 66667,
  "REV_AT_EPOCH": 3357,
  "BSTAR": 0.00014303,
  "MEAN_MOTION_DOT": 0.00004295,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	PELICAN-5
Operator	Planet Labs, Inc. (Planet)HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Nov 28, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	160HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/66667

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.