▸Orbital parameters

Orbit class	SSO
Inclination	97.1992°
Eccentricity	0.0000847
Period	93.5 min
Apogee	444 km
Perigee	443 km
Mean motion	15.40914436 rev/day
RAAN	263.6911°
Arg of perigee	99.4399°
Mean anomaly	260.6944°
B*	1.6525e-4
Rev at epoch	4,831

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 65316U 25188B 26187.67727808 .00006711 00000-0 16525-3 0 9991

2 65316 97.1992 263.6911 0000847 99.4399 260.6944 15.40914436 48314

▸ source OMM (JSON)

{
  "OBJECT_NAME": "PELICAN-4",
  "OBJECT_ID": "2025-188B",
  "EPOCH": "2026-07-06T16:15:16.826+00:00",
  "MEAN_MOTION": 15.40914436,
  "ECCENTRICITY": 0.0000847,
  "INCLINATION": 97.1992,
  "RA_OF_ASC_NODE": 263.6911,
  "ARG_OF_PERICENTER": 99.4399,
  "MEAN_ANOMALY": 260.6944,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 65316,
  "REV_AT_EPOCH": 4831,
  "BSTAR": 0.00016525,
  "MEAN_MOTION_DOT": 0.00006711,
  "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-4
Operator	Planet Labs, Inc. (Planet)HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Aug 26, 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/65316

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